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Design of a Novel Electromechanical Flight Control Actuation System with Configurable Redundancy for UAVs

Crossref DOI link: https://doi.org/10.1007/978-981-16-6328-4_7

Published Online: 2021-10-07

Published Print: 2022

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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